EP2898282A1 - Treibladungsansetzer, waffe und verfahren zum ansetzen von treibladungen - Google Patents
Treibladungsansetzer, waffe und verfahren zum ansetzen von treibladungenInfo
- Publication number
- EP2898282A1 EP2898282A1 EP13794798.2A EP13794798A EP2898282A1 EP 2898282 A1 EP2898282 A1 EP 2898282A1 EP 13794798 A EP13794798 A EP 13794798A EP 2898282 A1 EP2898282 A1 EP 2898282A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- propellant charge
- propellant
- weapon
- receptacle
- charges
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/01—Feeding of unbelted ammunition
- F41A9/06—Feeding of unbelted ammunition using cyclically moving conveyors, i.e. conveyors having ammunition pusher or carrier elements which are emptied or disengaged from the ammunition during the return stroke
- F41A9/09—Movable ammunition carriers or loading trays, e.g. for feeding from magazines
- F41A9/20—Movable ammunition carriers or loading trays, e.g. for feeding from magazines sliding, e.g. reciprocating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/37—Feeding two or more kinds of ammunition to the same gun; Feeding from two sides
- F41A9/375—Feeding propellant charges and projectiles as separate units
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/38—Loading arrangements, i.e. for bringing the ammunition into the firing position
- F41A9/39—Ramming arrangements
- F41A9/42—Rammers separate from breech-block
Definitions
- the invention relates to a propellant charge applicator for applying propellant charges in an elevatable weapon barrel having a propellant charge receptacle arranged on an elevation adjustment element, from which a plurality of propellant charges can be introduced along a setting direction into the weapon barrel.
- Another object of the invention is a weapon with an ultraviolet laser gun barrel and such propellant charge piecing.
- the invention relates to a method for applying propellant charges in an elevatable weapon barrel with a arranged on an elevation adjusting element propellant charge from which a plurality of propellant charges are introduced along a Ansetzraum in the barrel.
- propellant charge applicators are used, which have a propellant charge receptacle for receiving a plurality of propellant charge modules. Since the gun barrel is usually designed NASAbar, it is necessary to realize short loading times, the propellant charges to be set in different elevation directions of the gun barrel, resulting in special requirements for the corresponding propellant charge piecemeal.
- a propellant charge applicator is known from EP 1 483 544 B1, the propellant charge receptacle of which is arranged on a pivotably mounted elevation adjustment element. Via the elevation adjustment element, the position of the propellant charge receptacle can be adapted to the elevation direction position of the weapon barrel, so that the propellant charges can be set in different directions of the weapon.
- the elevation adjustment element is first pivoted into an elevation position, in which the weapon tube and the attachment direction of the propellant charge applicator are aligned parallel to one another. Subsequently, it is necessary to spend the propellant charge in the area behind the gun barrel, after which the gun barrel and the Ansetzraum aligned with each other and the propellant charges can then be introduced starting from this position in the gun barrel.
- a pivot arm is provided, via which the propellant charge recording can be spent in a pivoting movement from the area next to the weapon in their Ansetzwolf in the area behind the gun barrel. From this position, the propellant charges can then be introduced along the Ansetzraum in the barrel.
- the invention provides the invention, a propellant charge applicator, a weapon and a method for applying
- propellant charges which can be used even in confined spaces.
- this object is achieved by solving that the propellant charge receptacle is arranged to be translationally movable transversely to the attachment direction relative to the elevation adjustment element.
- the propellant charge intake Due to the translational movability of the propellant charge intake, it can be moved in a straight line relative to the elevation adjustment element from a position behind the weapon barrel to a position next to the weapon and vice versa.
- the movement of the propellant charge intake therefore requires a substantially lower space than is the case when pivoting the propellant charge, which is why the propellant charge can be used even in confined spaces.
- a structurally advantageous embodiment of the propellant charge applicator provides that the elevation adjusting element is designed in the manner of a pivoting jib. By pivoting the pivot arm, the orientation of the propellant charge recording the directional position of the gun barrel can be tracked.
- the elevation adjustment element is pivotable about a pivot axis extending horizontally.
- the elevation adjustment element can be directed in elevation around the horizontal pivot axis and thus the propellant charge can easily be readjusted.
- the pivot axis of the elevation adjustment element corresponds to the elevation direction. tachse the gun barrel, resulting in a coaxial arrangement. An offset between the pivot axes of the gun barrel and the elevation adjusting element is avoided, which has proved to be advantageous, especially in terms of control technology.
- the propellant charge receptacle is translationally movable via a movement means connected to the elevation adjustment element.
- the movement means together with the Treiblandungsauf would be directed via the elevation adjustment in elevation.
- the propellant charge uptake can be moved linearly with respect to the elevation adjustment element via the movement means, in particular in a direction parallel to the pivot axis of the elevation adjustment element, wherein the elevation movement and the transverse movement can also be superimposed for realizing short loading times.
- the propellant charge receptacle is designed to be movable in the attachment direction. Due to the movement of the propellant charge intake in the direction of attachment, the propellant charges can be brought from a lying behind a bottom piece of the weapon position directly to the cargo space of the weapon. In this case, the propellant charge intake can be moved up to the cargo space of the weapon by means of an opening provided in the bottom piece of the weapon, in order then to allow the propellant charge to be pushed out of the propellant charge into the weapon barrel.
- the movement means connected to the elevation adjustment element are arranged so as to be movable in the attachment direction along the elevation adjustment element.
- the mobility of the Movement means along the elevation readjustment element is advantageous insofar as the propellant charge can be moved via the movement means both transversely to the Ansetzides and in Ansetzraum.
- means are advantageously provided for increasing the relative speed of the propellant charge intake in the direction of attachment relative to the elevation adjuster. Via the means for increasing the relative speed, it can be achieved that the relative speed of the propellant charge receptacle relative to the elevation adjuster element in the attachment direction is greater than the corresponding relative speed of the motive means.
- the propellant charges taken up in the propellant charge intake can therefore be introduced into the weapon barrel with a speed that is greater in comparison to the movement of the motive means, as a result of which short attachment times can be achieved.
- the movement means has a lifting table for generating a lifting movement and a drive for actuating the lifting table.
- the propellant charge can be easily moved translationally.
- the propellant charge receptacle can be coupled to the lifting side of the lifting table, which is translationally movable relative to the drive side of the lifting table coupled to the drive.
- Embodiments of the propellant charge applicator will first be described below, which concern further details of the motive means before then discussing further aspects of the propellant charge applicator, such as a retainer and a guide plate.
- an embodiment is advantageous in which the drive is connected via switching means with the lifting table such that the Lifting table on the drive both actuated and linearly movable.
- the lifting table two independent movements can be performed.
- the lifting side of the lifting table coupled to the propellant charge receptacle can be moved translationally relative to the drive side coupled to the elevation adjusting element.
- the lift table can be moved linearly, wherein the lift side and the drive side are moved in a common direction. Since the actuation of the lifting table and the linear movement of the lifting table are carried out via the same drive, it is not necessary to provide a plurality of separate drives for actuating and moving the lifting table, resulting in an overall simple structure.
- connection of the drive with the lifting table is designed such that the lifting table is movable transversely to its stroke direction. In this way, coupled to the lifting side of the lifting table propellant charge recording can be moved in two independent spatial directions.
- connection of the drive with the lifting table is designed such that the lifting table is movable as a unit.
- the lift table can be actuated via the drive as well as moved linearly as a whole.
- connection of the drive with the lifting table is designed such that the lifting table is either actuated or movable.
- the drive can either move only the stroke side of the lift table in the stroke direction or linearly move the lift table as a unit.
- about the switching means can be switched between the actuation of the lifting table and the movement of the lifting table.
- the switching automatically in an end position of Lifting movement of the lifting table, so that it is not necessary to initiate the switching from the outside, for example via a control signal.
- the connection of the drive with the lifting table can be designed such that the lifting table can be actuated and moved simultaneously, as a result of which non-linear courses of movement of the lifting side of the lifting table can be realized.
- the lifting table has two scissor arms whose drive-side end is coupled to the switching means.
- the scissor arms can be pivotally connected to each other, so that over a pivoting movement of the scissor arms against each other, the lifting movement of the lifting table can be generated.
- the movement of the scissor arms can be controlled via the switching means coupled on the drive side.
- the drive-side end of a first scissor arm is translatorily fixed.
- the first scissor arm can be set translationally for actuating the lifting table, so that the pivoting of a second scissor arm relative to the first, fixed scissor arm triggers a lifting movement.
- the drive-side end of the second scissor arm is translationally movable. If the drive-side end of the first scissor arm is fixed, the scissors can be closed by translatory movement of the drive-side end of the second scissor arm and the lifting movement of the lifting table can be generated.
- the drive-side end of the second scissor arm is coupled via a spindle to the drive, so that the drive-side end of the second scissor arm can be moved translationally along the spindle.
- the definition of the drive-side end of the first scissor arm is detachably formed. By releasing the fixing, the drive-side end of the first scissor arm can be released for translational movement, whereby it is possible to move the lift table as a whole linearly.
- the ends of the scissor arms are designed for linear movement of the lifting table against each other fixable. After releasing the fixing of the drive-side end of the first scissor arm, the drive-side end of the first scissor arm can be fixed relative to the drive-side end of the second scissor arm. The drive-side ends of the scissor arms can then be moved together with a fixed distance translationally, so that the lifting table is moved linearly as a unit.
- the switching means comprise a first form-fitting element, in particular a claw, for fixing the first scissor arm to the drive side of the movement means.
- the first form-fitting element can be positively connected to the end of the first scissor arm or to an element connected to the end of the first scissor arm, for example a guide element, in order to translate the first scissor arm to a fixed point.
- the first scissor arm can be pivotably coupled to the guide element, so that the first scissor arm can be pivoted in spite of the translational fixing for actuating the lifting table.
- the switching means further comprise a second positive locking element, in particular also a claw, which is arranged to be movable together with the drive-side end of the second scissor arm.
- a second positive locking element in particular also a claw, which is arranged to be movable together with the drive-side end of the second scissor arm.
- the drive-side ends of the two scissor arms for linear movement of the lifting table can be coupled together.
- the second form-fitting element can be connected to the drive-side end of the first scissor arm or to an element connected to the end of the first scissor arm, for example a guide element, in the manner of a driver. In this case, however, the connection between the first positive-locking element and the first scissor arm must first be released.
- the first positive locking element can be latched to the first scissor arm.
- the latching via the second positive locking element is releasable.
- the second positive locking element can for this purpose be approximated to the first positive locking element in order thereby to release the latching of the first scissor arm.
- the retainer is pivotably articulated on the supply slide, so that the retainer can be activated with a pivoting movement.
- the retainer can be transferred from a retracted feed position into a set-up restraint position.
- the propellant charges can be introduced into the weapon barrel via the feed slider.
- the retainer In the erected restraint position, the retainer may protrude in the manner of a holding finger of the feed slider. In this position, the retainer protrudes into the cargo space of the weapon and the propellant charges are held by resting on the retainer in the cargo space of the weapon barrel.
- the retainer may be folded in the feed position such that it forms at least part of the thrust surface. In the restraint position, the retainer can project from the feed slider such that only the retainer but not the feed slider is in contact with the propellant charges.
- the retainer in particular via a spring, is biased in the direction of the retracted feed position. About the bias, the movement of the retainer can be generated in the direction of the feed position. It is therefore not necessary to provide drive elements for pivoting the retainer from the restraint position into the feed position.
- the retainer can be pivoted by an angle of more than 90 ° in order to transfer from the feed position to the retainer position.
- the retainer and the thrust surface of the feed slider may include an obtuse angle so that the retainer can not be pivoted back into the retracted feed position by the propellant charges applied against the retainer.
- the retainer protrudes beyond the propellant charge receptacle in the restraint position in the attachment direction. By the supernatant can be achieved that the retainer extends into the cargo space of the gun tube and can hold the propellant charges in the gun barrel.
- the feed slide is guided in a guide in the propellant charge receptacle. Through the guide, the feed slide can be forced in its movement in a linear movement path along the Ansetzrich- direction.
- an erection device via which the movement of the feed slider can be transferred in an erecting movement of the retainer.
- About the Aufstellin therapies can the movement the feed slide can be used to set up the retainer.
- the set-up device is preferably designed without drive, so that it is not necessary to provide a separate drive for setting up the retainer.
- the raising movement can be triggered via a triggering element arranged on the propellant charge receptacle.
- the triggering element can be arranged on the propellant charge receptacle in such a way that the raising movement is automatically triggered when the supply pusher reaches the triggering element.
- the trigger element is arranged in the end region of the feed path described by the feed movement of the feed slide, so that the raising movement of the retainer can be initiated in the end region of the feed path. It can thus be prevented that the retainer already sets up during the feed movement of the feed slide and possibly damage the propellant charges.
- a further advantageous embodiment provides that on the retainer, a coupling element, in particular a rope, is connected in such a way that the triggering element can engage in the coupling element for setting up the retainer.
- the coupling element can be jointly movable with the feed slide such that it interacts with the triggering element when the triggering element is reached and initiates the erection movement.
- the trigger element is designed in the manner of a roll. The moving rope can be caught and stretched over the roller. Due to the tension of the rope, the retainer can be set up. It has also proven to be advantageous if an overload protection is provided for the trigger element, so that an excessive force acting on the trigger element can not damage the trigger element.
- the triggering element is arranged movable in the direction of attachment against the force of a spring.
- the force acting on the trigger element can be damped.
- the triggering element can be arranged on a carrier which is movable relative to the propellant charge receptacle and which is mounted spring-damped.
- the propellant charge receptacle may have a guide for the propellant charges.
- the propellant charge applicator has a guide element for guiding the propellant charges when feeding in their set position, which is arranged in the direction of attachment relatively movable relative to the propellant charge recording.
- the propellant charge can be moved through a narrow opening in the end of the weapon up to the cargo space of the gun barrel zoom.
- the guide element can be moved backwards in the direction of attachment relative to the propellant charge receptacle such that the guide element remains outside of the end piece.
- the propellant charge applicator has a guide surface extending parallel to the attachment direction.
- the propellant charges moved in the direction of attachment can be guided in the direction of attachment via the guide surface.
- the guide element is movably mounted on a guide axis arranged parallel to the attachment direction. By movement along the guide axis, the guide element can be moved translationally parallel to the Ansetzraum.
- the guide element is arranged to pivot with respect to the propellant charge receptacle, so that the guide element for introducing propellant charges into the propellant charge receptacle can be pivoted relative to the propellant charge receptacle.
- the guide element is pivotally mounted about the guide axis.
- the guide shaft thus has a double function, since the guide axle serves as a guide for the movement in the direction of the attachment direction and at the same time as a bearing for the pivoting movement of the guide element relative to the drive load receptacle.
- the guide element is pivotable against the force of a spring, so that the guide element is always biased by the spring in the direction of the propellant charge received in the propellant charge recording.
- the guide element can be formed shell-shaped and adapted to the radius of the propellant charges such that a flat contact and thus good guidance results.
- the object is achieved by the propellant charge receptacle being arranged so as to be translationally movable transversely to the attachment direction relative to the elevation adjustment element.
- the propellant charge receptacle Due to the translational movability of the propellant charge receptacle, it can be moved in a straight line relative to the elevation adjustment element from a position behind the weapon barrel into a position next to the weapon and vice versa.
- the movement of the propellant charge intake therefore requires a much smaller space than is the case when pivoting the propellant charge, which is why the weapon is usable even in confined spaces.
- it contributes to the solution of the problem, when the arranged on the elevation adjusting element propellant charge transversely to the direction of attachment relative to the elevation readjustment element is moved translationally.
- the propellant charge intake Due to the translational movability of the propellant charge intake, it can be moved in a straight line relative to the elevation adjustment element from a position behind the weapon barrel to a position next to the weapon and vice versa.
- the movement of the propellant charge intake therefore requires a much smaller space than when pivoting the propellant charge of the Case is why the propellant charge can be used even in confined spaces.
- FIG. 2 shows a weapon with a propellant charge applicator according to FIG. 1 in a perspective view, a view corresponding to the representation in FIG. 2 viewed from the other side, the weapon according to FIG. 2 in perspective detail views 1 in a perspective view, in which the propellant charges are in their attached position in the cargo space of the weapon, to illustrate the piecing process, the propellant charge applicator of FIG. 1
- FIG. 10 is a detailed perspective view of the propellant charge according to the representation in Fig. 9, the Zugarschieber the propellant charge with deposited retainer in perspective view, a view corresponding to the representation in Fig. 1 1 viewed from the other side, the moving means of the propellant charge in perspective view, the movement means of FIG. 13 in perspective view to illustrate the processes in Solving the determination of the first scissor arm, one of the representation in Fig. 14a corresponding perspective view viewed from another direction, the movement means of FIG. 13 in perspective view to illustrate the movement of the lifting table, one of the representation in Fig. 15a corresponding perspective view in another direction,
- Fig. 16-18 a propellant charge applicator in various perspective
- large-caliber weapon 1 is shown with a gun only 101 sections shown.
- the weapon 1 can be arranged platform, for example, on a military vehicle or a mobile or stationary weapons.
- such weapon tubes 101 are mounted in a rotatable carriage, for example a revolving tower of a military vehicle. For straightening the weapon barrel 101 in elevation, this is mounted pivotably about an elevation direction axis E, which extends along a shield 105 of the weapon 1.
- the weapon 1 is operated with divided ammunition, which consists of the actual projectile and stored separately from the projectile propellant charges 8.
- the projectile and the propellant charges 8 are introduced separately into the weapon barrel 101 of the weapon, so that it is possible to select the quantity of propellant charge depending on the number of propellant charges 8 as a function of the situation.
- modular propellant charges 8 are used which have a cylindrical shape and can be plugged together in the axial direction.
- a propellant charge 2 is provided on the weapon 1, which is shown in detail in Fig. 1.
- the propellant charge converter 2 has a propellant charge receptacle 5, which is designed in the manner of a propellant charge shell and serves to receive a plurality of propellant charges 8. From the propellant charge intake 5, the propellant charges 8 can be introduced along the direction of attachment A into the weapon barrel 101. In order to be able to apply the propellant charges 8 independently of the elevation position of the weapon barrel 101, the propellant charge applicator 2 has a propellant charge receptacle 5, which tracks the elevation direction of the weapon barrel 101.
- the propellant charge receptacle 5 is for this purpose connected to an elevation adjustment element 3.
- the elevation adjustment element 3 is designed in the manner of a pivot arm, which is articulated on the pivot 105 of the weapon 1.
- the elevation adjustment element 3 is mounted pivotably about the elevation direction axis E of the weapon 1. Therefore, the position of the propellant charge recording 5 of elevation direction of the gun barrel 1 can be tracked so that the attachment of propellant charges 8 regardless of the directional position of the gun barrel 101 is possible. It is also possible, at the same time to direct the gun barrel 101 and still apply the propellant charges 8 during the directional movement, which can be implemented very fast firing.
- the propellant charge receptacle 5 can be pivoted via the elevation adjuster element 3 into a position in which the propellant charges. 5 would have a different position from the direction of the weapon 1, which will be explained in more detail below.
- the propellant charge converter 2 has a pivoting drive 300 which has a drive element 301 which can be telescoped by means of a drive motor 302. One end of the drive element 301 is connected to the elevation adjustment element 3 and the opposite end of the drive element 301 to the tower carrying the weapon 1.
- the elevation adjustment element 3 can be actuated and pivoted via the pivoting drive 300 independently of the weapon barrel 101.
- an axially movable feed pusher 6 is arranged on the propellant charge receptacle 5.
- the propellant charges 8 are conveyed along the direction of attachment A in the direction of the cargo space 103 of the weapon barrel 101, wherein the movement of the propellant charges 8 is guided via a guide element 7.
- a guide element 7 On the feed slider 8 and the guide member 7 will be discussed in more detail.
- the propellant charge receptacle 5 is in a position in the area next to the weapon 1. This position is taken to receive propellant charges 8 from a magazine or to release the area behind the gun barrel 101 for the return movement of the gun barrel 101. Because of the firing reaction forces occurring during the firing, a considerable recoil movement of the weapon barrel 101 and the bottom piece 102 of the weapon 1 arranged in the area behind the weapon barrel results in order to prevent damage to the propellant charge propeller 2 Propellant charge 5 therefore transferred before firing in the position shown in FIG. 2 and 3.
- the position of the propellant charge receptacle 5 is adjusted by pivoting the elevation adjustment element 3 to the elevation direction position of the weapon barrel 101. From the position shown in FIG. 4 next to the weapon 1 or next to the weapon barrel 101, the propellant charge receptacle 5 is subsequently moved into the position shown in FIG. 5 behind the weapon barrel 101. Starting from this position, the propellant charge receiver 5 is then moved in the direction of the Ansetzcardi A of the propellant charges 8. As can be seen in FIGS. 6 and 7, the propellant charge receptacle 5 is guided through an opening 104 of the bottom piece 102 as far as the cargo space of the weapon 1. In a further step, the propellant charges are then transported via the feed slide 6 in the cargo space, see. 8 and 9.
- the propellant charge receptacle 5 is arranged to be translationally movable transversely to the attachment direction A relative to the elevation adjustment element 3.
- the propellant charge receptacle 5 can be transferred directly in a straight line from the position behind the weapon barrel 101 into the position next to the weapon 1 and vice versa. This offers, in particular compared to solutions which pivot the propellant charge receptacle 5 away from the position. Provide the gun barrel 101 in the position next to the gun barrel 101, an advantage because only a substantially cubic space for the movement of the propellant charge receptacle 5 is required.
- the translatory movement of the propellant charge receiver 5 relative to the elevation adjuster element 3 takes place via a movement means 4 connected to the elevation adjuster element 3.
- the movement means 4 is connected to the elevation adjuster element 3 in such a way that the propellant charge intake 5 differs from that in FIG Fig. 4 shown position next to the weapon 1 linearly in the position shown in Fig. 5 can be transferred, from which the propellant charges 8 can be introduced in Ansetzraum A in the barrel 101.
- the moving means 4 has as an essential element a lifting table 400 for generating a lifting movement and a drive 410 for actuating the lifting table 400, which will be explained in more detail below with reference to the illustrations in FIGS. 4 to 9.
- the propellant charge intake 5 of the propellant charge converter 2 is initially in a position next to the weapon 1.
- the propellant charges 8 can be inserted by hand or via a supply automatic from a propellant charge magazine into the propellant charge receptacle 5.
- the guide element 7 is pivotably mounted on the propellant charge receptacle. me 5 hinged.
- the guide element 7 can be pivoted away laterally against the force of a spring 700 in order to provide the space required for inserting the propellant charges 8.
- a nose 701 is provided, over which the guide element 7 can be pivoted.
- the nose 701 may, for. B. interact with an opening element not shown in the figures.
- the movement means 4 is actuated.
- the lifting table 400 of the moving means 4 is extended via the drive 410.
- the arranged on the lifting side of the lifting table 400 propellant charge receptacle 5 is thereby translated in a small space in a direction of movement B moves, which is aligned perpendicular to the Ansetz- direction A of the propellant charges 8.
- the propellant charge receptacle 5 is then moved in Ansetzcardi A on the bottom piece 102 to.
- the movement means 4 is moved linearly along the elevation adjustment element 3.
- the moving means 4 or the lifting table 400 is moved as a unit together with the arranged on this propellant charge receptacle 5 in Ansetzraum A.
- the drive 410 is connected via the switching means to be described in more detail with the lifting table 400 such that the lifting table 400 via the drive 410 both actuated and linear, ie translational, is movable.
- the propellant charge converter 2 has only one drive 410 for movement of the propellant charge receptacle 5 in the direction of attachment A and transversely to the Ansetzraum A, resulting in a simple structure.
- the connection between the drive 410 and the lifting table 400 is designed such that the lifting table 400 is movable transversely to the stroke direction B.
- the lifting table 400 can be moved linearly as a unit via the drive 410.
- switching means are provided, via which the lifting table 400 is connected to the drive 410.
- the switching means for connecting the drive 410 with the lifting table 400 are designed such that the lifting table 400 is either actuated or movable, which will be discussed in more detail below.
- the propellant charge receptacle 5 is in a position in which it is partially driven into the bottom piece 102 through an opening 104 in the bottom piece 102.
- the propellant charge receptacle 5 In this position, the propellant charge receptacle 5 is moved up through the bottom piece 102 as far as the rear end of the weapon barrel 101, so that the drive charge receptacle 5 bears directly against the end of the weapon barrel 101. Starting from this position, the propellant charges 8 can be pushed over the feed slide 6 from the propellant charge receptacle 5 into the charge space 104. As can be seen from the illustrations in FIGS. 6 and 7, the propellant charge applicator 2 has a guide element 7, via which the propellant charges 8 are held and guided during their movement in the direction of attachment A in the propellant charge receptacle 5.
- the guide element 7 is arranged relative to the propellant charge receptacle 5 in the attachment direction A net, so that it can be moved when inserting the propellant charge receptacle 5 in the bottom piece 102 relative to the propellant charge receptacle 5 and thus remain outside of the bottom piece 102. Further details of the guide element 7 will be described in more detail.
- the feeding of the propellant charges 8 into their set position in the charge space 103 of the weapon barrel 101 takes place in the propellant charge applicator 2 via the supply slide 6 which is axially guided in the propellant charge receptacle 5 and which moves from the position shown in FIG. 6 at the rear end of the propellant charge accumulator 5 into the 8 and 9 shown position at the front, charge space side end of the propellant charge receptacle 5 is movable.
- the propellant charges 8 are pushed along the propellant charge receptacle 5 in Ansetzraum A in the cargo space.
- the propellant charges 8 are accelerated in such a way that they are brought into the charge space 103 of the weapon barrel 101, solely because of their inertia, without any further action of the feed pusher 6 beyond the charge chamber-side end of the propellant charge receptacle 5.
- a movably arranged retainer 601 is provided on the feed slider 6, via which the propellant charges 8 can be secured in position in their set position.
- the retainer 601 is pivotably coupled to the feed slider 6 about a pivot axis R.
- the pivot axis R is located at the upper end of the feed slider 6.
- the retainer 601 is oriented substantially perpendicular to the Ansetzraum A.
- the retainer 601 is formed overall fork-like and has two prongs 608, 609 on.
- the tines 608, 609 are arranged in the feed position such that they form an enlargement of the thrust surface of the feed slide 6.
- the enlargement is due to the fact that the tines 608, 609 are in the feed position in the area adjacent to the thrust surface of the feed slide 6.
- the retainer 601 may be transferred from the retracted feed position to the erected retainer position shown in FIG.
- the pivoting angle between the feed position and the retaining position of the retainer 601 is more than 90 °. This has the advantage that the propellant charge 8 applied to the retainer 601 can not pivot the retainer 601 out of the retaining position in the direction of its feed position.
- the propellant charge 8 is prevented from collapsing the retainer 601.
- the retainer 601 is further designed such that it protrudes forward in the restraint position on the propellant charge receptacle 5, see. It is therefore not necessary to move the feed slider 6 beyond the charge-space-side end of the propellant charge receiver 5 to hold the propellant charges 8 in the weapon barrel 101.
- an erection device is provided on the feed slide 6, via which the movement of the feed slide 6 in the application direction A can be converted into an erection movement of the retainer 601. This on adjusting device will be explained in more detail below, in particular with reference to the Fign.10-12.
- the feed slide 6 is guided in a guide 503 of the propellant charge receptacle 5 along the attachment direction A and moved via a threaded spindle 507. bar.
- the feed slide 6 has a guide slide 606 designed in the manner of a spindle nut, which is seated on the threaded spindle 507.
- the threaded spindle 507 is coupled to a drive 509, cf. Fig. 1 1 and 12.
- the drive 509 is firmly connected to the propellant charge receiving 5.
- a trigger element 504 is also arranged, via which the raising movement of the retainer 601 can be triggered.
- the triggering element 504 is designed in the manner of a roller, by means of which a coupling element 602 designed as a cable and connected to the retainer 601 can be caught in the direction of attachment A during the movement of the feeding slider 6.
- the coupling element 602 is connected to the retainer 601 in such a manner that the retainer 601 can be set up by pulling against the coupling element 602 against the force of a spring 603. As can be seen from FIG.
- the coupling element 602 is fixed at a connection point 605 to the retainer 601 and extends over a deflection roller 604 to a further connection point 607 on the guide slide 606 of the feed slide 6, cf.
- the triggering element 504 is arranged on the propellant charge receptacle 5 in such a way that it can engage in the cable 602 as soon as the cable 602 moved with the feed pusher 6 is moved into the region of the triggering element 504.
- the trigger element 504 captures the cable 602 as shown in FIGS. 11 and 12, pulls on the cable 602 due to the relative movement and thus sets the retainer 601 on.
- the trigger element 502 is arranged in the end region of the feed path. Furthermore, an overload protection for the trigger element 504 is provided. As can be seen from the illustration in FIG. 12, the trigger element 504 on the propellant charge receptacle 5 is not rigid, but movable against the force of a spring 506, arranged on the propellant charge receptacle 5. For this purpose, the trigger element 504 is arranged on a carrier 505, which is guided movably in the drive-up receptacle 5 in the attachment direction.
- the trigger element 504 is movable together with the carrier 505 in the direction of attachment A against the force of a spring 506, which is designed as a tension spring. As a result, the force is limited to the trigger element 504 or the force applied by this to the cable 602 force.
- the retainer 601 In order to transfer the retainer 601 back from the set-up restraint position to the feed position, the retainer 601 is pretensioned in the direction of the folded-in feed position.
- the bias is via a spring 603, which is designed in the manner of a torsion spring and is arranged coaxially to the pivot axis R of the retainer 601. Due to the bias, it is not necessary to provide a drive to move the retainer 601 from its retainer position to its feed position.
- the lift table 400 is formed as a scissors table.
- the lift table 400 has two scissor arms 401, 402 which are pivotally connected to each other and extend between a drive side and a lift side of the lift table 400.
- the stroke side of the Lifting table 400 is coupled to the propellant charge receiver 5 so that the propellant charge receiver 5 can be moved linearly with respect to the drive side of the lift table connected to the elevation adjuster 3.
- the stroke-side ends of the scissor arms 401 and 402 are each pivotally mounted in the propellant charge receptacle 5 in a slide bearing 403, 404.
- the slide bearings 403, 404 are arranged to be linearly movable in the propellant charge receptacle 5, so that the distance between the stroke-side ends of the scissor arms 401, 402 may change during the actuation of the lifting table 400.
- the scissor arms 401, 402 are designed in the manner of double scissor arms, which each have two parallel arranged, over several axes 423, 424 interconnected legs.
- the two legs of the second scissor arm 402 are connected by a plate 405.
- the drive-side ends of the scissor arms 401 and 402 are coupled to switching means 421, 422 to be described in more detail below, see FIG. 13.
- the drive-side end of the first scissor arm 401 is pivotable about an axle 423 stored.
- the axis 423 is connected via a fork-like strut 409 with a guide element 425, which is guided linearly in the elevation adjustment element 3.
- a locking element designed as a bolt 426 is provided, in which in the position shown in FIG. 13, a positive locking element 421 engages latching.
- the form-locking element 421 is designed in the manner of a claw, which surrounds the bolt 426.
- the interlocking element 421 is pivotally mounted in a bearing 308 which is fixedly connected to the elevation adjusting element 3.
- the drive-side end of the first view renarms 401 translationally defined with respect to the elevation adjustment element 3 become.
- the drive-side end of the second scissor arm 402 is designed translationally movable.
- the scissor arm 402 is connected via an axis 424 with a spindle nut 412, which is seated on a threaded spindle 411.
- the threaded spindle 411 is coupled to the drive 410.
- FIG. 14 a in which the lifting side of the lifting table 400 is arranged away from the elevation adjusting element 3.
- the drive-side ends of the scissor arms 401, 402 are in this position both in the region of an end face 304 of the elevation adjustment element 3.
- a side view in Fig. 14a corresponding plan view of the end face 304, Fig. 14b.
- the fixing of the driving-side end of the first scissor arm 401 can be solved to move the lift table 400 as a whole.
- the fixing of the first scissor arm 401 is achieved by the first positive locking element 421 via the second positive locking element 422.
- the second positive locking element 422 is biased by a spring 428 in a downwardly pivoted position.
- the second positive locking element 422 comes into contact with the first positive locking element 421.
- the first positive locking element 421 has an obliquely arranged control surface 429 which comes into contact with a bracket 432 of the second positive locking element.
- the positive-locking element 421 is set up in such a way that it is lifted off the bolt 426 of the guide element 425.
- the locking of the first mold closing element 421 with the bolt 426 is released.
- the first scissor arm 421 is thus released for translational movement.
- the second positive locking element 422 has a guide surface 430, which in the movement of the second
- Positive-locking element 422 slides in the direction of the first positive-locking element 421 via the bolt 426. As a result, the second positive locking element 422 is pivoted upwardly and locked with the bolt 426.
- the ends of the scissor arms 401, 402 are fixed against each other and can be moved translationally with a defined distance from each other.
- the lifting table 400 is moved via the drive 410 in the attachment direction A.
- the movement of the ends of the scissor arms 401, 402 is guided on the drive side via the threaded spindle 411.
- the lift table 400 is pulled from the position shown in Fig. 14a to a position Fig. 15a.
- the illustration in FIG. 15b shows a view corresponding to FIG. 15a on the end face 304 of the elevation adjustment element 3. It can be seen that the form-fit element 422 is in engagement with the bolt 426 of the guide element 425.
- the drive-side end of the first scissor arm 401 is thus moved via the second positive-locking element 422 in the direction of the drive 410.
- the released first positive locking element 421 is biased by a spring 427 such that it is pressed in a downwardly pivoted position, see. Fig. 15a.
- the second positive locking element 422 is performed with its control surface 430 on the temple 431 of the first positive locking element 421, whereby the second
- Positive locking element 422 is pivoted upwards and thus the locking of the second positive locking element 422 is solved with the bolt 426.
- the first positive locking element 421 is guided via its control surface 429 via the bolt 426 and pivoted upwards.
- the positive-locking element 421 latches with the bolt 426 and fixes the drive-side end of the first scissor arm 421 to the elevation adjustment element 3.
- the propellant charge receptacle 5 is movably arranged in the attachment direction A on the elevation adjustment element 3.
- means for increasing the relative speed are provided in the propellant charge applicator 2, which are to be described in detail below.
- the relative speed is increased in the case of the propellant charge applicator 2 according to the exemplary embodiment via ropes 451 and 452 arranged between the elevation adjuster element 3 and the propellant charge intake 5, which are shown in detail in FIGS. 19 and 20.
- the first cable 451 is used to accelerate the propellant charge absorption 5 in Ansetzraum A.
- the second cable 452 is provided to increase the speed of the propellant charge receptacle 5 against the Ansetzraum A.
- the first cable 451 is connected to a connection point 501 on the propellant charge receiver 5.
- the cable 451 extends over a guide roller 457 on the slide bearing 404 of the second scissor arm 402 in the propellant charge receiver 5 via a guide roller 455 in the region of the pivot axis of the scissor arms 401 and 402 to another guide roller 453 in the region of the end of the first scissor arm 401, see.
- the cable 451 extends parallel to the threaded spindle 41 1 of the movement means 4 to a connection point 305 in the region of the end face 304 of the elevation adjustment element 3.
- About the cable 451 can speed doubling the propellant charge 5 with respect to the elevation adjustment 3 in the movement of the lifting table 400 take place in Ansetzraum.
- the second cable 452 is connected to the propellant charge receptacle 5 at a connection point 502, cf. Fig. 20.
- the cable 452 extends from the connection point 502 via a deflection roller in the region of the sliding bearing 404 of the second scissor arm 402 via a guide roller 456 in the region of the pivot axis of the pivot arms 401 and 402 to a guide roller 454 in the region of the end of the first scissor arm 401st , see. Fig. 15b.
- the cable 452 furthermore runs parallel to the drive spindle 41 1 in the direction of the drive 410.
- the attachment point of the second cable 452 lies in the region of the drive 410 on the elevation adjustment element 3 and is concealed in the figures.
- the speed of the propellant charge receptacle 5 can be doubled with respect to the elevation adjuster element 3 in the movement counter to the attachment direction A.
- the guide element 7 is designed as a shell-shaped overall.
- the guide element 7 has a guide surface 702, which runs parallel to the Ansetzraum A.
- the propellant charges can be guided along the guide surface 702 guided in the direction of the gun barrel 101.
- the propellant charges 8 received in the propellant charge receptacle 5 can be secured in position during the movement of the propellant charge receptacle 5 from a position next to the weapon 1 to a position behind the weapon 1 via the guide element 7.
- the guide element 7 is movably mounted on a guide axis F arranged parallel to the attachment direction A, so that the guide element 7 moves in the direction of the propellant charge receptacle 5 in the direction of the Charge space 103 is shifted relative to the propellant charge receptacle 5 to the rear.
- the guide element 7 is arranged pivotably about this guide axis F on the propellant charge receptacle 5.
- the guide element 7 can be pivoted relative to the propellant charge receptacle 5 in order to introduce propellant charges 8 into the propellant charge receptacle 5.
- the guide element 7 is biased by a spring 700 so that the guide element 7 is pressed onto the propellant charges 8 received in the propellant charge receptacle 5.
- the weapon 1 described above and the propellant charge applicator 2 for attaching propellant charges 8 into the elevatable weapon barrel 101 of the weapon 1 have a propellant charge receptacle 5, which is arranged transversely to the attachment direction A relative to the elevation adjuster 3 in a translationally movable manner.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Manipulator (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE201210108832 DE102012108832A1 (de) | 2012-09-19 | 2012-09-19 | Treibladungsansetzer, Waffe und Verfahren zum Ansetzen von Treibladungen |
| PCT/DE2013/100336 WO2014044255A1 (de) | 2012-09-19 | 2013-09-18 | Treibladungsansetzer, waffe und verfahren zum ansetzen von treibladungen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2898282A1 true EP2898282A1 (de) | 2015-07-29 |
| EP2898282B1 EP2898282B1 (de) | 2017-01-04 |
Family
ID=49626775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP13794798.2A Active EP2898282B1 (de) | 2012-09-19 | 2013-09-18 | Treibladungsansetzer, waffe und verfahren zum ansetzen von treibladungen |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP2898282B1 (de) |
| DE (1) | DE102012108832A1 (de) |
| ES (1) | ES2614882T3 (de) |
| WO (1) | WO2014044255A1 (de) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102017107442B4 (de) | 2017-04-06 | 2021-03-18 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Vorrichtung zum Laden einer Rohrwaffe mit Munitionskörpern |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR566410A (fr) * | 1922-08-08 | 1924-02-14 | Schneider & Cie | Appareil de chargement et de refoulement des projectiles pour bouches à feu |
| US4278008A (en) * | 1979-10-12 | 1981-07-14 | The United States Of America As Represented By The Secretary Of The Army | Separate loading ammunition automatic cannon |
| DE3118383A1 (de) * | 1981-05-09 | 1982-11-25 | Rheinmetall GmbH, 4000 Düsseldorf | Ladeeinrichtung fuer eine automatische querverschluss-rohrwaffe |
| DE3931059A1 (de) * | 1989-09-18 | 1991-03-28 | Rheinmetall Gmbh | Treibladungs-portionierer fuer eine mengenvariabel beladbare ladeschale |
| DE3932130A1 (de) * | 1989-09-27 | 1991-04-04 | Rheinmetall Gmbh | Ladevorrichtung fuer modulare treibladung |
| SE503489C2 (sv) * | 1994-10-13 | 1996-06-24 | Bofors Ab | Ansättningssystem |
| SE507935C2 (sv) * | 1996-12-02 | 1998-07-27 | Bofors Ab | Sätt och anordning för frammatning av valfria granater ur fallschaktsmagasin |
| SE513006C2 (sv) * | 1999-01-20 | 2000-06-19 | Bofors Weapon Sys Ab | Sätt och anordning för att hantera artillerigranater vid laddning av artilleripjäser |
| US6481328B1 (en) * | 2000-01-05 | 2002-11-19 | Bofors Defense Ab | Method and device for handling propellant charges |
| DE10258263B4 (de) * | 2002-12-13 | 2006-01-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Schießmodul |
-
2012
- 2012-09-19 DE DE201210108832 patent/DE102012108832A1/de not_active Withdrawn
-
2013
- 2013-09-18 ES ES13794798.2T patent/ES2614882T3/es active Active
- 2013-09-18 WO PCT/DE2013/100336 patent/WO2014044255A1/de not_active Ceased
- 2013-09-18 EP EP13794798.2A patent/EP2898282B1/de active Active
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2014044255A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2014044255A1 (de) | 2014-03-27 |
| EP2898282B1 (de) | 2017-01-04 |
| DE102012108832A1 (de) | 2014-03-20 |
| ES2614882T3 (es) | 2017-06-02 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE102009035277B4 (de) | Bohrvorrichtung | |
| WO2015139879A1 (de) | STROMABNEHMERSYSTEM MIT TELESKOPARM FÜR KRANE, CONTAINERKRANE, ERTGs UND FÖRDEREINRICHTUNGEN | |
| EP0450373B1 (de) | Vorrichtung zum Laden von Rohrwaffen, insbesondere von Panzerhaubitzen | |
| EP2875305B1 (de) | Waffenplattform, militärisches fahrzeug mit einer waffenplattform und verfahren zum betrieb einer waffenplattform | |
| WO2012159140A1 (de) | Befestigungsvorrichtung zum befestigen einer frontblende an einer schublade | |
| EP4077852B1 (de) | Verriegelungsvorrichtung zur lösbaren verriegelung zweier relativ zueinander bewegbarer möbelteile | |
| DE2818279C2 (de) | Vorrichtung zum automatischen Fördern und/oder Laden von großkalibriger, patronierter Munition | |
| EP2898281B1 (de) | Treibladungsansetzer, waffe und verfahren zum ansetzen von treibladungen | |
| EP4077844A1 (de) | Anordnung zur führung einer schiebetür oder falt-schiebetür | |
| DE1627730A1 (de) | Vorrichtung fuer den Zusammenbau von Muttern und Unterlegscheiben od.dgl. mit Schraubenbolzen od.dgl. | |
| EP0640805B1 (de) | Geschosszuführungsvorrichtung für eine Panzerhaubitze | |
| DE1140109B (de) | Ladevorrichtung fuer Geschuetze | |
| DE3839496C2 (de) | ||
| EP2898282B1 (de) | Treibladungsansetzer, waffe und verfahren zum ansetzen von treibladungen | |
| DE102010043207B4 (de) | Anhänger | |
| DE69206698T2 (de) | Automatische Munitionszuführvorrichtung für Panzerkanonen | |
| EP0406716A1 (de) | Geschosstransporter, insbesondere für ein Kampffahrzeug | |
| EP2898280B1 (de) | Vorrichtung mit einem hubtisch und treibladungsansetzer | |
| EP1736726B1 (de) | Treibladungszuführungssystem | |
| EP0766056A2 (de) | Sicherheitsvorrichtung für einen Zündstift einer Feuerwaffe | |
| DE2044920A1 (de) | Bolzensetzgerät mit Kartuschenmagazin | |
| CH649626A5 (de) | Einstosseinrichtung. | |
| EP4621341A1 (de) | Primermagazin-wechselvorrichtung mit schwenkarm | |
| EP4621340A2 (de) | Primermagazin-wechselbaugruppe | |
| EP4621342A1 (de) | Primermagazin-wechselvorrichtung mit greifvorrichtung |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 20150317 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| AX | Request for extension of the european patent |
Extension state: BA ME |
|
| DAX | Request for extension of the european patent (deleted) | ||
| 17Q | First examination report despatched |
Effective date: 20160405 |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| INTG | Intention to grant announced |
Effective date: 20161019 |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 859662 Country of ref document: AT Kind code of ref document: T Effective date: 20170115 |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502013006007 Country of ref document: DE |
|
| REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
| REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D Ref country code: NL Ref legal event code: MP Effective date: 20170104 |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2614882 Country of ref document: ES Kind code of ref document: T3 Effective date: 20170602 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170405 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170404 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170504 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170504 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170404 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 5 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502013006007 Country of ref document: DE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
| REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20170930 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170918 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170918 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170930 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20130918 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 859662 Country of ref document: AT Kind code of ref document: T Effective date: 20180918 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180918 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170104 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20220922 Year of fee payment: 10 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20220920 Year of fee payment: 10 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20220930 Year of fee payment: 10 Ref country code: ES Payment date: 20221018 Year of fee payment: 10 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20220928 Year of fee payment: 10 |
|
| P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230527 |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL Ref country code: SE Ref legal event code: EUG |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230930 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230930 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230930 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 502013006007 Country of ref document: DE Owner name: KNDS DEUTSCHLAND GMBH & CO. KG, DE Free format text: FORMER OWNER: KRAUSS-MAFFEI WEGMANN GMBH & CO. KG, 80997 MUENCHEN, DE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230919 |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20241104 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230918 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230918 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230919 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230919 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20250930 Year of fee payment: 13 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20250923 Year of fee payment: 13 |